Bulletproof and explosion-proof type unmanned aerial vehicle command and control square cabin

Abstract

The utility model relates to the technical field of unmanned aerial vehicle transfer control, in particular to a bulletproof and explosion-proof type unmanned aerial vehicle command and control square cabin which comprises a cabin body and an explosion-proof cabin door arranged on the cabin body. The cabin body comprises a first bulletproof steel plate, a plurality of first frameworks arranged on the inner side of the first bulletproof steel plate at intervals, first PVC thermal bridge plates arranged on the inner sides of the first frameworks, first heat preservation plates arranged between every two adjacent first frameworks, and first inner panels connected with the inner sides of the first heat preservation plates and the inner sides of the first PVC thermal bridge plates. The explosion-proof cabin door comprises a door frame profile arranged between the two first frameworks, an explosion-proof door leaf hinged to the door frame profile and matched with the door opening, and a plurality of hinge assemblies arranged on the door frame profile and the explosion-proof door leaf. By means of the structure, firm protection of the square cabin when the square cabin faces bullet attack, mine explosion and other threats is guaranteed, the heat preservation efficiency in the cabin is remarkably improved, and therefore the common welding deformation problem and the defect that the heat preservation performance is insufficient of a traditional square cabin are overcome.

Description

Technical Field

[0001] This utility model relates to the field of drone transfer and control technology, specifically a bulletproof and explosion-proof drone command and control cabin. Background Technology

[0002] In the field of modular shelters, general military modular shelters are constructed in accordance with national military standards such as GJB6109-2007 "General Specifications for Military Modular Shelters" and GJB5017-2003 "Technical Requirements for Weapon and Equipment Maintenance Modular Shelters." Standard modular shelter walls are constructed by hot-pressing and bonding inner and outer panels, a wall frame, thermal bridge plates, and insulation boards. The inner and outer panels can be made of aluminum, steel, carbon fiber, fiberglass, or other materials. The frame is made of aluminum, steel, or non-metallic materials. Modular shelters constructed from these materials do not provide bulletproof or mine-proof protection.

[0003] Current drone command and control modules only have drone command and control functions and do not have bulletproof and explosion-proof functions. Some modules with bulletproof functions are generally made by adding composite materials such as ceramic, fiber-based, and Kevlar to the module wall panels. There are many process problems in the design and manufacturing of the module. Using bulletproof steel plates as the main modules of the module can meet the bulletproof and explosion-proof functions, but there are problems such as welding deformation of the module and insufficient thermal insulation of the module. Utility Model Content

[0004] The purpose of this utility model is to provide a bulletproof and explosion-proof UAV command and control container to solve the problems of existing UAV command and control containers that only have command functions and lack bulletproof and explosion-proof properties; containers reinforced with composite materials such as ceramic and fiber matrix have manufacturing difficulties; and bulletproof steel plates, although bulletproof and explosion-proof, are prone to deformation and have poor thermal insulation.

[0005] To achieve the above objectives, this utility model provides the following technical solution: a bulletproof and explosion-proof unmanned aerial vehicle (UAV) command and control cabin, comprising a cabin body and an explosion-proof door disposed on the cabin body; the cabin body comprises a first bulletproof steel plate, a plurality of first frames arranged at intervals on the inner side of the first bulletproof steel plate, a first PVC thermal bridge plate disposed on the inner side of the first frames, a first insulation board disposed between two adjacent first frames, and a first inner panel connected to the inner side of the plurality of first insulation boards and the plurality of first PVC thermal bridge plates; the first bulletproof steel plate is provided with a door opening; the explosion-proof door comprises a door frame profile disposed between two first frames, an explosion-proof door leaf hinged to the door frame profile and matching the door opening, and a plurality of hinge components disposed on the door frame profile and the explosion-proof door leaf.

[0006] Furthermore, the explosion-proof door leaf includes a second bulletproof steel plate, a door leaf profile, two second frames, a second PVC thermal bridge plate, and a second insulation board. The two second frames are connected to the inner wall of the door leaf profile and one side is connected to the inner side of the second bulletproof steel plate. The second PVC thermal bridge plate is connected to one side of the second frames. The second insulation board is connected to the other side of the two second frames and to the inner side of the second bulletproof steel plate.

[0007] Furthermore, both the first and second bulletproof steel plates are provided with a plurality of spaced circular holes, and the interior of the circular holes is provided with ordinary steel plates; the hinge assembly includes a hinge member provided on the first and second bulletproof steel plates, and a plurality of rivets provided on the hinge member and threadedly engaged with the first and second bulletproof steel plates.

[0008] Furthermore, a sealing strip is provided between the door leaf profile and the door frame profile.

[0009] Furthermore, the cabin is equipped with a partition, which forms a front cabin and a rear cabin; the explosion-proof door includes a first door on one side of the rear cabin, a double door on one end of the rear cabin, and a second door on one side of the front cabin, the second door being equipped with louvers.

[0010] Furthermore, the rear compartment is equipped with generators and batteries arranged at intervals, the inside of the second compartment door is equipped with grounding rods and fire extinguishers arranged at intervals, and the upper side of the rear compartment is equipped with an electric roof.

[0011] Furthermore, a drone transport sliding mechanism is provided on the lower interior side of the front cabin and near the double doors; the drone transport sliding mechanism includes a trolley rail located on the lower interior side of the front cabin, an ST mechanical trolley that slides with the trolley rail, tray holders located at the four upper corners of the ST mechanical trolley, and multiple drone landing gear holders located on the ST mechanical trolley.

[0012] Furthermore, the forward compartment is equipped with equipment components, including an electric exhaust fan located on one side of the forward compartment and spaced apart from the first door; an electric ventilation fan and an escape window located on the other side of the forward compartment and spaced apart; a heater and a bulletproof window located on one side of the forward compartment and spaced apart; an emergency light, an anti-static device, and a charger located on one side of the forward compartment and spaced apart in sequence; a top air conditioner located on the upper side of the forward compartment; a pan-tilt camera located on the upper side of the forward compartment; multiple cable reels located on the lower side of the forward compartment; two control panels located on the lower side of the forward compartment and connected to one side of the bulkhead; a cabinet located on the lower side of the forward compartment and between the two control panels; explosion-proof seats located on the lower side of the forward compartment and corresponding to the two control panels; and multiple civil engineering tools located on the inner wall of the first door. The first door is located between the emergency light and the anti-static device. The charger is located above the electric exhaust fan, and the heater is located diagonally above the electric exhaust fan.

[0013] Furthermore, the front cabin has two spaced-apart drone propeller supports on one side of its interior. The drone propeller supports are located above the electric ventilation fan and on the side of the heater. The drone propeller supports include a mounting plate connected to the interior side of the front cabin, an inclined platform connected to one side of the mounting plate, multiple inclined grooves arranged longitudinally on the inclined platform, and a connecting cover hinged to one side of the inclined platform and corresponding to the inclined grooves.

[0014] Compared with the prior art, the beneficial effects of this utility model are as follows:

[0015] This utility model discloses a bulletproof and explosion-proof UAV command and control container. Its container structure includes a first bulletproof steel plate, a first frame, a first PVC thermal bridge plate, a first insulation board, and a first inner panel, and is equipped with an explosion-proof door with explosion-proof, bulletproof, and heat-insulating properties. Together, they form a container that has both heat-insulating performance and meets stringent safety standards. This structure not only ensures the container's robust protection against threats such as bullet attacks and landmine explosions, but also significantly improves the heat insulation performance inside the container, thereby overcoming the common welding deformation problems and insufficient heat insulation performance defects of traditional containers. Attached Figure Description

[0016] Figure 1 This is a side view of the bulletproof and explosion-proof UAV command and control cabin of this utility model;

[0017] Figure 2 This is a top view schematic diagram of the bulletproof and explosion-proof UAV command and control cabin of this utility model;

[0018] Figure 3 This is a side view of the bulletproof and explosion-proof UAV command and control cabin of this utility model;

[0019] Figure 4 For the present utility model Figure 3 Enlarged structural diagram;

[0020] Figure 5 This is a cross-sectional schematic diagram of the cabin of this utility model;

[0021] Figure 6 This is a cross-sectional schematic diagram of the doorway of this utility model;

[0022] Figure 7 This is a top view schematic diagram of the internal layout of the bulletproof and explosion-proof UAV command and control cabin of this utility model;

[0023] Figure 8 This is a side view of the internal layout of the bulletproof and explosion-proof UAV command and control cabin of this utility model.

[0024] Figure 9 This is a side view of the internal layout of the bulletproof and explosion-proof UAV command and control cabin of this utility model.

[0025] Figure 10 This is a side view of the control panel of this utility model;

[0026] Figure 11 This is a schematic diagram of the structure of the drone propeller support of this utility model.

[0027] In the diagram: 1. Hull; 2. First hatch; 3. Second hatch; 4. Double door; 5. Second bulletproof steel plate; 6. Electric exhaust fan; 7. Escape window; 8. Electric roof cover; 9. Bulkhead; 10. Front compartment; 11. Rear compartment; 12. First bulletproof steel plate; 13. First frame; 14. First PVC thermal bridge plate; 15. First insulation board; 16. First inner panel; 17. Doorway; 18. Door frame profile; 19. Door leaf profile; 20. Second frame; 21. Second PVC thermal bridge plate; 22. Second insulation board; 23. Hinge; 24. Circular hole; 25. Ordinary steel plate; 26. Rivet; 27. Sealing 28. Pan-tilt camera; 29. ​​Top air conditioner; 30. Cart slide rail; 31. ST mechanical cart; 32. Pallet holder; 33. UAV landing gear holder; 34. Cable reel; 35. Control panel; 36. Cabinet; 37. Generator; 38. Battery; 39. UAV propeller bracket; 40. Heater; 41. Bulletproof window; 42. Fire extinguisher; 43. Civil tools; 44. Grounding rod; 45. Charger; 46. Static eliminator; 47. Emergency light; 48. Mounting plate; 49. Tilting platform; 50. Tilting groove; 51. Connecting cover; 52. Electric ventilation fan; 53. Explosion-proof seat. Detailed Implementation

[0028] Please see Figure 1-11A bulletproof and explosion-proof unmanned aerial vehicle (UAV) command and control container includes a container body 1 and an explosion-proof door mounted on the container body 1. The container body 1 includes a first bulletproof steel plate 12, multiple spaced first frames 13 welded to the inner side of the first bulletproof steel plate 12, first PVC thermal bridge plates 14 riveted to the inner side of the first frames 13, a first insulation board 15 disposed between two adjacent first frames 13, and a first inner panel 16 connected to the inner side of the multiple first insulation boards 15 and the multiple first PVC thermal bridge plates 14. The first bulletproof steel plate 12 has a door opening 17. The explosion-proof door includes a door frame profile 18 disposed between two first frames 13 and a... The door frame profile 18 is hinged to an explosion-proof door leaf that matches the door opening 17; multiple hinge components are installed on the door frame profile 18 and the explosion-proof door leaf; a 40×40×2mm square steel tube is used as the first frame 13, a 10mm thick PVC board is used as the first PVC thermal bridge plate 14, and a 50mm thick rigid polyurethane foam board is used as the first insulation board 15; finally, a special structural adhesive is sprayed to bond the first inner panel 16, and a wall covering is bonded to the inner wall of the first inner panel 16 to form a container with bulletproof and explosion-proof functions and good thermal insulation performance; when the container body 1 is installed, the container body 1 consists of a 9mm thick top and bottom plate, a thick... The outer shell is formed by welding the first bulletproof steel plate 12 with a side end plate of 15mm in diameter. The internal structure is installed in the following order: welding the first frame 13, bonding the first PVC thermal bridge plate 14 with structural adhesive and rivets 26, filling with the first insulation board 15, and finally spraying special structural adhesive to bond the inner panel. The inner wall is then bonded with wall fabric to form a container with bulletproof and explosion-proof functions and good insulation performance. The design of the first frame 13 avoids the weld seams of the bulletproof steel plate. A doorway 17 is opened in the first bulletproof steel plate 12, and an explosion-proof door leaf for explosion-proof, bulletproof, and insulation is installed through multiple hinged components. Before cold-pressing bonding, some electrical cables are pre-embedded, and conduits are used to reduce bends. Based on the characteristics of deformation of the major surfaces of the first bulletproof steel plate 12, the first frame 13 avoids deformation and weld seams, ensuring that the first frame 13 does not affect the flatness of the first inner panel 16. This solves the problem that deformation of the various surfaces of the cabin 1 welded from the first bulletproof steel plate 12 affects the installation of the insulation layer and the cabin 1 has insufficient insulation. According to the cold pressing bonding process, a cabin 1 with good insulation performance is formed. The cabin 1 composed of this structure meets the basic safety requirements of the cabin 1, such as bulletproof and mineproof, and also meets the insulation requirements of the cabin 1, solving the problems of welding deformation and insufficient insulation of the existing cabin.

[0029] The explosion-proof door leaf includes a second bulletproof steel plate 5, a door leaf profile 19, two second frames 20, a second PVC thermal bridge plate 21, and a second insulation board 22. The two second frames 20 are connected to the inner wall of the door leaf profile 19 and one side is connected to the inner side of the second bulletproof steel plate 5. The second PVC thermal bridge plate 21 is connected to one side of the second frames 20. The second insulation board 22 is connected to the other side of the two second frames 20 and to the inner side of the second bulletproof steel plate 5. Through the structural composition of the explosion-proof door leaf, the explosion-proof door leaf simultaneously has explosion-proof, bulletproof, and heat-insulating properties.

[0030] The first bulletproof steel plate 12 and the second bulletproof steel plate 5 are each provided with a plurality of spaced circular holes 24, and the interior of the circular holes 24 is provided with ordinary steel plate 25; the hinge assembly includes a hinge 23 provided on the first bulletproof steel plate 12 and the second bulletproof steel plate 5, and a plurality of rivets 26 provided on the hinge 23 and threadedly engaged with the first bulletproof steel plate 12 and the second bulletproof steel plate 5; in view of the technical difficulties in installing the explosion-proof hatch due to the deformation of the door opening 17 and the high hardness of the first bulletproof steel plate 12 and the second bulletproof steel plate 5, which makes it difficult to drill and tap the rivets 26, the first step is to address the technical difficulties in installing the explosion-proof hatch based on the following: The dimensions of the reserved door opening 17 determine the dimensions of the explosion-proof hatch. The positions of the rivet 26 mounting holes on the second bulletproof steel plate 5, the lock hole on the explosion-proof hatch, and the rivet 26 mounting holes on the first bulletproof steel plate 12 are determined in advance, and circular holes 24 are pre-drilled using a laser cutting machine. Then, ordinary steel plates 25 are welded and sealed before drilling and tapping for installation. To prevent water leakage, sealant is applied around the holes of the rivet 26 and the joints between the hatch body 1 and the door frame profile 18. This solves the technical problem of installing the hatch due to the deformation of the door opening 17 and the inability to drill holes on the first bulletproof steel plate 12 and the second bulletproof steel plate 5.

[0031] A sealing strip 27 is provided between the door leaf profile 19 and the door frame profile 18 to ensure airtightness.

[0032] The cabin 1 is equipped with a partition 9, which forms a front cabin 10 and a rear cabin 11. The explosion-proof doors include a first door 2 on one side of the rear cabin 11, a double door 4 at one end of the rear cabin 11, and a second door 3 on one side of the front cabin 10. The second door 3 is equipped with louvers. The double door 4 at one end of the rear cabin 11 facilitates the entry and exit of the drone from the cabin 1.

[0033] The rear cabin 11 is equipped with a generator 37 and a battery 38 arranged at intervals. The inner side of the second cabin door 3 is equipped with a grounding rod 44 and a fire extinguisher 42 arranged at intervals. The upper side of the rear cabin 11 is equipped with an electric top cover 8. By opening the electric top cover 8, the UAV data link antenna can be raised to the outside of the cabin 1 via the lifting mechanism.

[0034] A drone transport sliding mechanism is provided on the lower interior side of the front cabin 10, near the double doors 4. This mechanism includes a trolley rail 30 located on the lower interior side of the front cabin 10, an ST mechanical trolley 31 that slides along the trolley rail 30, pallet holders 32 located at the four upper corners of the ST mechanical trolley 31, and multiple drone landing gear holders 33 on the ST mechanical trolley 31. The ST mechanical trolley 31 can move along the trolley rail 30. The drone is secured to the ST mechanical trolley 31 by the multiple drone landing gear holders 33, and the ST mechanical trolley 31 can be moved via the pallet holders 32. 2. Once fixed in a designated position within the cabin 1 and securely locked, the pallet holder 32 provides sufficient force to secure the ST mechanical cart 31 and the drone within the cabin 1, preventing movement during transport. Even if the cabin 1 tilts at a large angle or overturns, the drone will not shift or tip over. Furthermore, the drone sliding mechanism facilitates the storage and convenient transport of the drone into and out of the cabin 1. To facilitate pushing the drone onto the ST mechanical cart 31, an easily detachable small ramp is provided at the rear of the ST mechanical cart 31. After pushing the drone onto the ST mechanical cart 31, the ramp can be removed and stored separately.

[0035] The forward compartment 10 is equipped with equipment components, including an electric exhaust fan 6 located on one side of the forward compartment 10 and spaced apart from the first door 2; an electric ventilation fan 52 and an escape window 7 located on the other side of the forward compartment 10; a heater 40 and a bulletproof window 41 located on one side of the interior of the forward compartment 10 and spaced apart; an emergency light 47, an electrostatic eliminator 46, and a charger 45 located on one side of the interior of the forward compartment 10 and spaced apart; a top air conditioner 29 located on the upper side of the forward compartment 10; a pan-tilt camera 28 located on the upper side of the interior of the forward compartment 10; multiple cable reels 34 located on the lower side of the interior of the forward compartment 10; and two spaced-apart control panels 35 located on the lower side of the interior of the forward compartment 10 and connected to one side of the bulkhead 9. The container includes a cabinet 36 located on the lower side of the front compartment 10, between two control panels 35; explosion-proof seats 53 located on the lower side of the front compartment 10, corresponding to the two control panels 35; and multiple civil engineering tools 43 mounted on the inner wall of the first door 2. The first door 2 is located between an emergency light 47 and an electrostatic eliminator 46. A charger 45 is located above an electric exhaust fan 6, and a heater 40 is located diagonally above the electric exhaust fan 6. The structural design of the two control panels 35 and the cabinet 36 fully considers ergonomic factors. The overall shape and the position and size of each facility and equipment should meet the comfort of the operators, providing two workstations. To meet the needs of personnel safety and secondary protection, explosion-proof seats 53 are provided. Through the layout and arrangement of the equipment components, the container 1 is fully functional, rationally designed, and easy to operate.

[0036] Two spaced-apart drone propeller supports 39 are provided on one side of the interior of the front cabin 10. The drone propeller supports 39 are located above the electric ventilation fan 52 and on the side of the heater 40. The drone propeller supports 39 include a mounting plate 48 connected to one side of the interior of the front cabin 10, a tilting platform 49 connected to one side of the mounting plate 48, multiple tilting grooves 50 arranged longitudinally on the tilting platform 49, and a connecting cover 51 hinged to one side of the tilting platform 49 and corresponding to the tilting grooves 50. The drone propeller supports 39 are designed according to the propeller size. Based on the arrangement of multiple tilting grooves 50, the drone propellers are placed in a slanted slot, which is conducive to the removal and placement of the propellers. The four propellers are installed compactly. The locking device on the connecting cover 51 adopts a combination of wing screw and magnet, making it convenient and quick to remove and place the drone propellers.

[0037] Working principle: During the installation of the cabin 1, the cabin 1 is composed of a 9mm thick top and bottom plate and a 15mm thick side end plate, welded together to form an outer shell of first bulletproof steel plate 12. The interior is installed in the following order: welding the first frame 13, bonding the first PVC thermal bridge plate 14 with structural adhesive and rivets 26, filling the first insulation board 15, and finally spraying special structural adhesive to bond the inner panel. The inner wall is bonded with wall cloth to form a cabin with bulletproof and explosion-proof functions and good thermal insulation performance. The design of the first frame 13 avoids the weld seams of the bulletproof steel plate. A door opening 17 is opened in the first bulletproof steel plate 12. An explosion-proof door leaf for explosion-proof, bulletproof and thermal insulation is installed through multiple hinge components. When installing the explosion-proof door leaf, the size of the explosion-proof cabin door is first determined according to the size of the reserved door opening 17. The positions of the rivet 26 mounting holes on the second bulletproof steel plate 5, the lock hole on the explosion-proof cabin door, and the rivet 26 mounting holes on the first bulletproof steel plate 12 are determined in advance and rounded in advance with a laser cutting machine. The door frame profile 18 is installed in the door opening 17 through the rivet 26 via the shaped hole 24. Then, the ordinary steel plate 25 is welded and sealed, and then holes are drilled and tapped. The explosion-proof door leaf is installed through the hinge 23 and multiple rivets 26. Before cold pressing and bonding, some electrical cables are pre-embedded and the conduit is used to reduce the number of bends. According to the characteristics of the deformation of the major surfaces of the first bulletproof steel plate 12, the first frame 13 avoids the deformation and weld seams to ensure that the first frame 13 does not affect the flatness of the first inner panel 16. This solves the problem that the deformation of the various surfaces of the cabin 1 caused by the first bulletproof steel plate 12 affects the installation of the insulation layer and the insufficient insulation of the cabin 1. According to the cold pressing and bonding process, the cabin 1 with good insulation performance is formed. The cabin 1 composed of this structure meets the basic safety requirements of the cabin 1, such as bulletproof and landmine protection, and also meets the insulation requirements of the cabin 1. This solves the problems of welding deformation and insufficient insulation of the existing cabin.

[0038] The above are merely preferred embodiments of the present utility model and are not intended to limit the present utility model. Any modifications, equivalent substitutions, and improvements made within the spirit and principles of the present utility model should be included within the protection scope of the present utility model.

Claims

1. A bulletproof and explosion-proof command and control container for unmanned aerial vehicles, characterized in that, The device includes a cabin (1) and an explosion-proof door on the cabin (1). The cabin (1) includes a first bulletproof steel plate (12), a plurality of first frames (13) arranged at intervals on the inner side of the first bulletproof steel plate (12), a first PVC thermal bridge plate (14) on the inner side of the first frame (13), a first insulation plate (15) between two adjacent first frames (13), and a first inner panel (16) connected to the inner side of the plurality of first insulation plates (15) and the plurality of first PVC thermal bridge plates (14). The first bulletproof steel plate (12) is provided with a door opening (17). The explosion-proof door includes a door frame profile (18) between two first frames (13), an explosion-proof door leaf that is hinged to the door frame profile (18) and matches the door opening (17), and a plurality of hinge components on the door frame profile (18) and the explosion-proof door leaf.

2. The bulletproof and explosion-proof command and control container for unmanned aerial vehicles as described in claim 1, characterized in that, The explosion-proof door leaf includes a second bulletproof steel plate (5), a door leaf profile (19), two second frames (20), a second PVC thermal bridge plate (21), and a second insulation board (22). The two second frames (20) are connected to the inner wall of the door leaf profile (19) and one side is connected to the inner side of the second bulletproof steel plate (5). The second PVC thermal bridge plate (21) is connected to one side of the second frame (20). The second insulation board (22) is connected to the other side of the two second frames (20) and to the inner side of the second bulletproof steel plate (5).

3. The bulletproof and explosion-proof command and control container for unmanned aerial vehicles as described in claim 2, characterized in that, The first bulletproof steel plate (12) and the second bulletproof steel plate (5) are provided with a plurality of spaced circular holes (24), and the inside of the circular holes (24) is provided with ordinary steel plate (25); the hinge assembly includes a hinge (23) provided on the first bulletproof steel plate (12) and the second bulletproof steel plate (5), and a plurality of rivets (26) provided on the hinge (23) and threadedly engaged with the first bulletproof steel plate (12) and the second bulletproof steel plate (5).

4. The bulletproof and explosion-proof command and control container for unmanned aerial vehicles as described in claim 2, characterized in that, A sealing strip (27) is provided between the door leaf profile (19) and the door frame profile (18).

5. The bulletproof and explosion-proof command and control container for unmanned aerial vehicles as described in claim 1, characterized in that, The cabin (1) is provided with a partition (9), and the cabin (1) is formed into a front cabin (10) and a rear cabin (11) through the partition (9); the explosion-proof door includes a first door (2) on one side of the rear cabin (11), a double door (4) on one end of the rear cabin (11), and a second door (3) on one side of the front cabin (10), and the second door (3) is provided with louvers.

6. The bulletproof and explosion-proof command and control container for unmanned aerial vehicles as described in claim 5, characterized in that, The rear compartment (11) is equipped with a generator (37) and a battery (38) arranged at intervals. The inner side of the second door (3) is equipped with a grounding rod (44) and a fire extinguisher (42) arranged at intervals. The upper side of the rear compartment (11) is equipped with an electric top cover (8).

7. A bulletproof and explosion-proof unmanned aerial vehicle (UAV) command and control container as described in claim 5, characterized in that, The front cabin (10) is provided with a drone transport sliding mechanism on the lower side of the interior and near the double door (4). The drone transport sliding mechanism includes a trolley rail (30) located on the lower side of the interior of the front cabin (10), an ST mechanical trolley (31) that slides with the trolley rail (30), tray holders (32) located at the four corners of the upper side of the ST mechanical trolley (31), and multiple drone landing gear holders (33) located on the ST mechanical trolley (31).

8. The bulletproof and explosion-proof command and control container for unmanned aerial vehicles as described in claim 5, characterized in that, The front cabin (10) is equipped with equipment components, including an electric exhaust fan (6) located on one side of the front cabin (10) and spaced apart from the first cabin door (2), an electric ventilation fan (52) and an escape window (7) located on the other side of the front cabin (10) at intervals, a heater (40) and a bulletproof window (41) located on one side of the front cabin (10) at intervals, an emergency light (47) and an electrostatic eliminator (46) and a charger (45) located on one side of the front cabin (10) at intervals, a top air conditioner (29) located on the upper side of the front cabin (10), a pan-tilt camera (28) located on the upper side of the front cabin (10), and a camera located inside the front cabin (10). Multiple cable reels (34) on the lower side, two spaced control panels (35) located on the lower side inside the front cabin (10) and connected to one side of the partition (9), a cabinet (36) located on the lower side inside the front cabin (10) and between the two control panels (35), explosion-proof seats (53) located on the lower side inside the front cabin (10) and respectively corresponding to the two control panels (35), multiple civil engineering tools (43) on the inner wall of the first door (2), the first door (2) is located between the emergency light (47) and the static eliminator (46), the charger (45) is located above the electric exhaust fan (6), and the heater (40) is located diagonally above the electric exhaust fan (6).

9. A bulletproof and explosion-proof command and control container for unmanned aerial vehicles as described in claim 8, characterized in that, The front cabin (10) has two spaced drone propeller supports (39) on one side of its interior. The drone propeller supports (39) are located above the electric ventilation fan (52) and on the side of the heater (40). The drone propeller supports (39) include a mounting plate (48) connected to one side of the front cabin (10), an inclined platform (49) connected to one side of the mounting plate (48), a plurality of inclined grooves (50) arranged longitudinally on the inclined platform (49), and a connecting cover (51) hinged to one side of the inclined platform (49) and arranged corresponding to the inclined grooves (50).

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